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Automatic Parameter Tuning for the Morpheus Vehicle Using Particle Swarm OptimizationA high fidelity simulation using a PC based Trick framework has been developed for Johnson Space Center's Morpheus test bed flight vehicle. There is an iterative development loop of refining and testing the hardware, refining the software, comparing the software simulation to hardware performance and adjusting either or both the hardware and the simulation to extract the best performance from the hardware as well as the most realistic representation of the hardware from the software. A Particle Swarm Optimization (PSO) based technique has been developed that increases speed and accuracy of the iterative development cycle. Parameters in software can be automatically tuned to make the simulation match real world subsystem data from test flights. Special considerations for scale, linearity, discontinuities, can be all but ignored with this technique, allowing fast turnaround both for simulation tune up to match hardware changes as well as during the test and validation phase to help identify hardware issues. Software models with insufficient control authority to match hardware test data can be immediately identified and using this technique requires very little to no specialized knowledge of optimization, freeing model developers to concentrate on spacecraft engineering. Integration of the PSO into the Morpheus development cycle will be discussed as well as a case study highlighting the tool's effectiveness.
Document ID
20130014605
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
Birge, B.
(L-3 Communications Corp. Houston, TX, United States)
Date Acquired
December 9, 2013
Publication Date
August 19, 2013
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
JSC-CN-28933
Report Number: JSC-CN-28933
Meeting Information
Meeting: AIAA Modeling and Simulation Technologies Conference
Location: Boston, MA
Country: United States
Start Date: August 19, 2013
End Date: August 22, 2013
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Public Use Permitted.
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